Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift

Author:	Morrow, John D
Year:	1955
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3548
Link:	https://digital.library.unt.edu/ark:/67531/metadc57805/